GB2585474B - A method and apparatus for producing at least part of a structural frame of a vehicle - Google Patents
A method and apparatus for producing at least part of a structural frame of a vehicle Download PDFInfo
- Publication number
- GB2585474B GB2585474B GB2006785.6A GB202006785A GB2585474B GB 2585474 B GB2585474 B GB 2585474B GB 202006785 A GB202006785 A GB 202006785A GB 2585474 B GB2585474 B GB 2585474B
- Authority
- GB
- United Kingdom
- Prior art keywords
- vehicle
- producing
- structural frame
- structural
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Automatic Assembly (AREA)
- Body Structure For Vehicles (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19275069.3A EP3741685A1 (en) | 2019-05-23 | 2019-05-23 | A method and apparatus for producing at least part of a structural frame of a vehicle |
GBGB1907299.0A GB201907299D0 (en) | 2019-05-23 | 2019-05-23 | A method and apparatus for producing at least part of a structural frame of a vehicle |
Publications (3)
Publication Number | Publication Date |
---|---|
GB202006785D0 GB202006785D0 (en) | 2020-06-24 |
GB2585474A GB2585474A (en) | 2021-01-13 |
GB2585474B true GB2585474B (en) | 2022-02-16 |
Family
ID=70736787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2006785.6A Active GB2585474B (en) | 2019-05-23 | 2020-05-07 | A method and apparatus for producing at least part of a structural frame of a vehicle |
Country Status (6)
Country | Link |
---|---|
US (1) | US11731788B2 (en) |
EP (1) | EP3972903A1 (en) |
JP (1) | JP7282924B2 (en) |
GB (1) | GB2585474B (en) |
SA (1) | SA521430933B1 (en) |
WO (1) | WO2020234565A1 (en) |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB170727A (en) * | 1920-08-23 | 1921-11-03 | Dermot Joseph Mooney | Improvements in metal spars, longerons or the like for aircraft |
GB309110A (en) * | 1928-01-03 | 1929-04-03 | Bristol Aeroplane Co Ltd | Improvements in or relating to light metal structures |
Family Cites Families (42)
Publication number | Priority date | Publication date | Assignee | Title |
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JPS6464740A (en) * | 1987-04-14 | 1989-03-10 | Northrop Corp | Built-up data model system |
US5106290A (en) * | 1987-04-14 | 1992-04-21 | Northrop Corporation | Assembly data model tool system |
US4956764A (en) * | 1987-04-14 | 1990-09-11 | Northrop Corporation | Assembly data model tool system |
US4945488A (en) * | 1987-04-14 | 1990-07-31 | Northrop Corporation | Integrated aircraft manufacturing system |
DE3805093C1 (en) | 1988-02-18 | 1989-03-09 | Siebler Verpackungstechnik Gmbh & Co Kg, 7537 Remchingen, De | |
JPH028699U (en) * | 1988-06-30 | 1990-01-19 | ||
US5516545A (en) | 1991-03-26 | 1996-05-14 | Sandock; Leonard R. | Coating processes and apparatus |
CA2554189C (en) | 1996-03-22 | 2010-08-03 | The Boeing Company | Determinant wing assembly |
GB0002837D0 (en) | 2000-02-08 | 2000-03-29 | British Aerospace | Assembling composite structures |
US6922599B2 (en) | 2001-08-13 | 2005-07-26 | The Boeing Company | System and method for producing an assembly by directly implementing three-dimensional computer-aided design component definitions |
US7410352B2 (en) | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
GB0519364D0 (en) | 2005-09-22 | 2005-11-02 | Airbus Uk Ltd | Assembly of aircraft components |
JP4513663B2 (en) | 2005-06-15 | 2010-07-28 | 富士電機ホールディングス株式会社 | Operation teaching method of assembly mechanism in automatic assembly system |
US7756321B2 (en) | 2007-02-28 | 2010-07-13 | The Boeing Company | Method for fitting part assemblies |
US7787979B2 (en) | 2007-03-14 | 2010-08-31 | The Boeing Company | Splicing fuselage sections without shims |
US8523110B2 (en) * | 2007-03-28 | 2013-09-03 | Airbus Operations Gmbh | Door frame component of cast titanium and structural fuselage part |
US20080254403A1 (en) | 2007-04-10 | 2008-10-16 | Jack Keith Hilliard | System for cnc-machining fixtures to set orthodontic archwires |
GB0720702D0 (en) | 2007-10-23 | 2007-12-05 | Airbus Uk Ltd | A shim for arrangement against a structural component and a method making a shim |
US8126688B2 (en) | 2008-11-05 | 2012-02-28 | The Boeing Company | Method and apparatus for identifying gaps between parts |
FR2946024B1 (en) * | 2009-05-27 | 2011-07-22 | Airbus France | INSTALLATION FOR CARRYING OUT AN AIRCRAFT FUSELAGE TRUNK |
US8634950B2 (en) | 2009-12-14 | 2014-01-21 | Embraer S.A. | Automated positioning and alignment method and system for aircraft structures using robots |
JP3169646U (en) * | 2011-05-29 | 2011-08-11 | 正臣 天野 | Wing production jig |
GB2498977B (en) | 2012-02-01 | 2015-10-07 | Bae Systems Plc | Drilling apparatus and method |
US9649820B1 (en) * | 2012-02-08 | 2017-05-16 | Textron Innovations, Inc. | Assembly using skeleton structure |
US9278763B2 (en) | 2013-01-15 | 2016-03-08 | The Boeing Company | Method and system for identifying fastener placement zones |
WO2015038041A1 (en) * | 2013-09-11 | 2015-03-19 | Saab Ab | A fixture device for manufacture of aeronautical structures and a method for applying the device |
EP2853963A1 (en) | 2013-09-30 | 2015-04-01 | BAE Systems PLC | Object production |
FR3016606B1 (en) * | 2014-01-21 | 2016-02-19 | Airbus Operations Sas | METHOD FOR MANUFACTURING A PART OF A FUSELAGE OF AN AIRCRAFT AND TOOLS FOR CARRYING OUT SAID METHOD |
US9990446B2 (en) | 2014-04-15 | 2018-06-05 | The Boeing Company | Predictive shimming for flexible surfaces |
GB201407182D0 (en) | 2014-04-24 | 2014-06-11 | Bae Systems Plc | Aircraft airframe assembly |
JP6464740B2 (en) | 2014-12-26 | 2019-02-06 | 三菱マテリアル株式会社 | Copper alloy for electronic and electrical equipment, copper alloy sheet for electronic and electrical equipment, parts for electronic and electrical equipment, terminals and bus bars |
US9925625B2 (en) | 2015-05-04 | 2018-03-27 | The Boeing Company | Assembly of an aircraft structure assembly without shimming, locating fixtures or final-hole-size drill jigs |
GB2541182B (en) | 2015-08-05 | 2021-03-03 | Bae Systems Plc | Aircraft part assembly |
US10275565B2 (en) | 2015-11-06 | 2019-04-30 | The Boeing Company | Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning |
EP3210757B1 (en) | 2016-02-24 | 2019-09-11 | Airbus Operations GmbH | Method of installing a fixture on a structure by additive manufacturing |
EP3210758B1 (en) | 2016-02-24 | 2019-12-11 | Airbus Operations GmbH | Method of installing a fixture |
US10450053B2 (en) | 2016-05-11 | 2019-10-22 | The Boeing Company | Methods using predictive shimming to optimize part-to-part alignment |
US10139808B2 (en) | 2016-09-07 | 2018-11-27 | The Boeing Company | Predictive shimming of joints |
US10303154B2 (en) | 2016-10-11 | 2019-05-28 | The Boeing Company | Surface based hole target for use with systems and methods for determining a position and a vector of a hole formed in a workpiece |
EP3535341A1 (en) | 2016-11-03 | 2019-09-11 | 3M Innovative Properties Company | Polythiol sealant compositions |
US11174041B2 (en) | 2018-06-14 | 2021-11-16 | The Boeing Company | Systems and methods for determining fasteners |
GB2576411B (en) * | 2018-06-28 | 2021-08-04 | Bae Systems Plc | Method and apparatus for assembling aircraft airframes |
-
2020
- 2020-05-07 EP EP20725895.5A patent/EP3972903A1/en active Pending
- 2020-05-07 JP JP2021569481A patent/JP7282924B2/en active Active
- 2020-05-07 US US17/607,626 patent/US11731788B2/en active Active
- 2020-05-07 WO PCT/GB2020/051119 patent/WO2020234565A1/en unknown
- 2020-05-07 GB GB2006785.6A patent/GB2585474B/en active Active
-
2021
- 2021-11-23 SA SA521430933A patent/SA521430933B1/en unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB170727A (en) * | 1920-08-23 | 1921-11-03 | Dermot Joseph Mooney | Improvements in metal spars, longerons or the like for aircraft |
GB309110A (en) * | 1928-01-03 | 1929-04-03 | Bristol Aeroplane Co Ltd | Improvements in or relating to light metal structures |
Also Published As
Publication number | Publication date |
---|---|
JP2022533776A (en) | 2022-07-25 |
WO2020234565A1 (en) | 2020-11-26 |
GB202006785D0 (en) | 2020-06-24 |
US20220204183A1 (en) | 2022-06-30 |
GB2585474A (en) | 2021-01-13 |
US11731788B2 (en) | 2023-08-22 |
SA521430933B1 (en) | 2023-02-20 |
JP7282924B2 (en) | 2023-05-29 |
EP3972903A1 (en) | 2022-03-30 |
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